DocumentCode
2310451
Title
LFT-based uncertainty modelling and μ-analysis of the HIRM+ RIDE flight control law
Author
Kureemun, Ridwan ; Bates, Declan G.
Author_Institution
Dept. of Eng., Leicester Univ., UK
fYear
2002
fDate
18-20 Sept. 2002
Firstpage
242
Lastpage
247
Abstract
This paper considers the problem of generating LFT-based uncertainty models for the robustness analysis of the HIRM+ aircraft using the structured singular value μ. Robustness properties of the RIDE controller are evaluated according to criteria currently in use by the European aircraft industry for the clearance of flight control laws. The proposed analysis approach is shown to be both rigorous and efficient, and demonstrates increased potential for automation of the flight clearance task.
Keywords
aircraft control; control system analysis; robust control; singular value decomposition; transforms; uncertain systems; μ-analysis; HIRM+ RIDE flight control law; HIRM+ aircraft; LFT-based uncertainty modelling; flight control law clearance; linear fractional transformation; Aerospace control; Automatic control; Frequency; Instruments; Mathematical model; Military aircraft; Robust control; Stability; Testing; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Aided Control System Design, 2002. Proceedings. 2002 IEEE International Symposium on
Print_ISBN
0-7803-7388-X
Type
conf
DOI
10.1109/CACSD.2002.1036961
Filename
1036961
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